Hub-shaft bolted-joint connection of a wind turbine
Abstract
A wind turbine includes a nacelle, a generator housed with the nacelle, a rotor having a rotatable hub with at least one rotor blade mounted thereto, at least one shaft rotatably coupled to the hub for driving the generator, and a rotor lock arranged with the shaft(s) for locking the shaft(s) in a locked position. The wind turbine also includes a bolted-joint connection at an interface between the hub and the shaft(s). The bolted-joint connection includes a first plurality of fasteners extending through the hub, the shaft(s), and the rotor lock. As such, a load transfer path from the hub to the shaft(s) travels through each of the hub, the shaft(s), and the rotor lock so as to increase a load capacity of the interface.
Claims
exact text as granted — not AI-modified1 . A wind turbine, comprising:
a nacelle; a generator housed with the nacelle; a rotor comprising a rotatable hub with at least one rotor blade mounted thereto; at least one shaft rotatably coupled to the hub for driving the generator; and a rotor lock arranged with the at least one shaft for locking the at least one shaft in a locked position; and a bolted-joint connection at an interface between the hub and the at least one shaft comprising a first plurality of fasteners extending through the hub, the at least one shaft, and the rotor lock, wherein a load transfer path from the hub to the at least one shaft travels through each of the hub, the at least one shaft, and the rotor lock so as to increase a load capacity of the interface.
2 . The wind turbine of claim 1 , further comprising a gearbox, wherein the at least one shaft comprises a rotor shaft rotatably coupled to the rotatable hub for driving the gearbox and a generator shaft rotatably coupled to the gearbox for driving the generator.
3 . The wind turbine of claim 2 , wherein the rotor lock is one of a rotor shaft rotor lock or a generator shaft rotor lock.
4 . The wind turbine of claim 1 , wherein the interface further comprises a hub stiffener.
5 . The wind turbine of claim 4 , wherein the hub stiffener is positioned on a rotor side of the rotor lock.
6 . The wind turbine of claim 4 , wherein the hub stiffener is positioned on a generator side of the rotor lock.
7 . The wind turbine of claim 4 , wherein the hub stiffener comprises a plurality of stiffener segments arranged circumferentially around the rotor lock.
8 . The wind turbine of claim 7 , wherein each of the plurality of stiffener segments receives one or more of the first plurality of fasteners therethrough.
9 . The wind turbine of claim 8 , wherein each of the plurality of stiffener segments is positioned within the rotatable hub.
10 . The wind turbine of claim 7 , wherein each of the plurality of stiffener segments receives a subset of a second plurality of fasteners therethrough such that the second plurality of fasteners secure the plurality of stiffener segments to the rotatable hub between the rotor lock and the hub, wherein the second plurality of fasteners is arranged concentric with the first plurality of fasteners.
11 . The wind turbine of claim 10 , wherein one or more of the subset of the second plurality of fasteners received through each of the plurality of stiffener segments comprises jacking components.
12 . The wind turbine of claim 11 , wherein the jacking components are positioned at opposing ends of the each of the plurality of stiffener segments.
13 . The wind turbine of claim 10 , wherein one or more of the plurality of stiffener segments comprises a scalloped portion for reducing weight thereof.
14 . A method of increasing a load capacity of an interface between a hub and a rotor shaft of a wind turbine, the method comprising:
providing a first plurality of fasteners through the hub, the rotor shaft, and a rotor lock of the wind turbine, the rotor lock comprising a first plurality of through holes; machining a second plurality of through holes through the rotor lock and through the hub; arranging a plurality of stiffener segments circumferentially between the rotor lock and the hub to form a hub stiffener, each of the plurality of stiffener segments comprising a plurality of through holes that align with a subset of the second plurality of through holes; and securing the hub stiffener between the rotor lock and the hub via a plurality of second fasteners that extend through the plurality of through holes of each of the stiffener segments and the second plurality of through holes of the rotor lock.
15 . The method of claim 14 , further comprising removing a shroud of the rotor lock before machining the second plurality of through holes through the rotor lock.
16 . The method of claim 14 , further comprising adjusting a height of the hub stiffener via one or more jacking components arranged with one or more of the plurality of stiffener segments to match a gap between the hub and the rotor lock.
17 . The method of claim 14 , further comprising installing a segmented rain cover at the interface.
18 . The method of claim 14 , further comprising machining the second plurality of through holes through the rotor lock from outside of the hub.
19 . The method of claim 14 , further comprising machining the second plurality of through holes through the rotor lock from within the hub.
20 . The method of claim 14 , wherein the second plurality of fasteners is arranged concentric with the first plurality of fasteners.Join the waitlist — get patent alerts
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